THE 


FLYING BOAT 
HANDBOOK 

NAVY DEPARTMENT 
BUREAU OF CONSTRUCTION AND REPAIR 


DECEMBER, 1918 


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THE 

F-5L FLYING BOAT 
HANDBOOK 


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NAVY DEPARTMENT 

BUREAU OF CONSTRUCTION AND REPAIR 


DECEMBER, 1918 



WASHINGTON 

GOVERNMENT PRINTING OFFICE 
1918 





V 






FIG. 1.—COMPLETE ASSEMBLY. 
































TABLE OF CONTENTS. 


. Page. 

List of illustrations. 7 

I. Specifications: 

1. General dimensions. 11 

2. Areas. H 

3 . Motors. 11 

4 . Tank capacities. 12 

5 . Endurance. 12 

6. Weights. 12 

II. Instructions for assembling: 

1. Shipment. 19 

2. Handling boxes. 19 

3 . Opening boxes and unpacking. 20 

4 . Examination of parts. 20 

(a) Hull. 21 

(b) Panels and tail. 21 

(c) General. 22 

5 . Assembly of center section. 22 

6. Assembly of outer wing panels. 24 

7 . Assembly of tail surfaces. 26 

8. General information.. . 27 

III. Packing sheets. 31 

IV. Tables. 43 

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FIG. 2.— METHOD OF LIFTING HULL CASE. 
Note.—Each sling is made of 1" by 66' AA strand cable. 
























































































































FIG. 3.—JIG FOR LIFTING PANELS. 













































Figu: 

No. 

i 

I 

i 

( 

ii 

u 

is 

12 

14 

15 

16 

17 

18 

19 

20 

21 

22 

23 

24 

25 

26 

27 

28 

29 

30 

31 

32 

33 

34 

35 

36 

37 


Facing 

page. 

5 

6 

7 

8 

9 

9 

12 

12 

back. 

back. 

back. 

back. 

back. 

back. 

back. 

back. 

back. 

13 

13 

14 

15 

15 

16 

16 

17 

17 

20 

21 

22 

23 

23 

24 

24 

25 

26 

26 

27 


LIST OF ILLUSTRATIONS. 


Title. 


Complete assembly. 

Method of lifting hull case. 

Jig for lifting panels. 

Method of panel erection. 

Level for dihedral angle. 

Bevel board for dihedral angle. 

Jig for leveling hull. 

Jig for longitudinal alignment of hull. 

General dimensions. 

Diagram of numbering of struts... 

Wiring diagram of panels. 

Tail unit assembly.. 

Lubrication chart—motor control. 

Lubrication chart of surface control. 

Diagram of Delco ignition system. 

Wiring and motor controls. 

Gasoline lines. 

Method of bracing hull case. 

Stenciling on hull case. 

Hull in case before shipment. 

Bracing hull in case. 

Fin edge bed of hull case. 

Hull bed of case.. 

Three-quarter view of hull resting on case bed 

Slipknot in lifting rope. 

Method of tilting hull. 

Placing hull on cradle.. 

Method of arranging lifting ropes. 

Packing case for engine foundations, etc. 

Method of lifting cases. 

Method of lifting panels out of packing case... 
Detachable sidewalk panel, partly removed... 

Splice in sidewalk beam. 

Sidewalk panel removed. 

Three-quarter view of cradle. 

Spark and throttle controls of port motor. 

New type of bomb signal disk. 

( 7 ) 

























































jure 

io. 

38 

39 

40 

41 

42 

43 

44 

45 

46 

47 

48 

49 

50 

51 

52 

53 

54 

55 

56 

57 


8 

LIST OF ILLUSTRATIONS— Continued. 


Title. 


Facing 

page. 


Rudder foot control. 

Instrument board. 

Interior view of forward gunner’s pit. 

Instrument board. 

Starboard switchboard. 

Looking aft over fuel tanks. 

Three-quarter view, looking aft over fuel tanks 

Gasoline manifold. 

After cockpit.-. 

Hull interior—forward section. 

Tail brace assembly.. 

Side view of bomb sight. 

Top view of bomb sight. 

Bow gun mount. 

Rear gun mount. 

Motor, oil and water piping.... 

Three-quarter view of center section.. 

Front view of complete assembly. 

Staging for wing assembly. 

Ordnance installation. 


27 

28 
29 
29 

32 

33 

34 

35 

35 

36 

37 

38 

39 

40 

40 

41 

44 

45 

46 
back. 







































































































































Adjusting Nut 
5ection At A-A 

FIG. 5.—ADJUSTABLE LEVEL FOR DIHEDRAL ANGLE. 


Insert- spirit Uve-l or rest spiril level on \oip 


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FIG. 6—BEVEL BOARD FOR DIHEDRAL ANGLE. 
























































PART I 


SPECIFICATIONS 


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F-5L FLYING BOAT HANDBOOK. 

SPECIFICATIONS. 


1. GENERAL DIMENSIONS. 

Overall upper wing. 103 feet 9* inches. 

Overall lower wing. 74 f ee t 3 f inches. 

Chord. 8 feet. 

Gap (C. L. of beams). 8 feet 10* inches. 

Stagger of wings. 0 °. 

Sweepback of wings.. 0 °. 

Dihedral angle... 1° 30 L 

Angle of incidence, horizontal stabilizer. 2 ° 3 (K. 

Angle of incidence, wings. 4 ° O'. 

Overall length of boat. 49 feet inches. 

Overall height of boat. 18 feet 9 £ inches. 

Wing curve. Modified R. A. F. 6 . 

2. AREAS. 

Square feet. 

Wing surfaces. 1 , 278. 0 

Ailerons. 119 . 0 


Total supporting surface. 1 , 397 . 0 


Horizontal stabilizer. 120. 9 

Vertical stabilizer. 34 . 7 

Rudder. 33. 5 

Elevators (2)... 55.3 

Nonskid fins (2). 31.1 

3. MOTORS. 

Two Liberty 45° Vee, 4-cycle, 12-cylinder 

.horsepower per motor (rated)_330 

( 11 ) 



























12 

4. TANK CAPACITIES. Pounds . 

Gasoline, 495 gallons, at 6.25 pounds per gallon. 3, 094 

Oil, 34 gallons, at 7.5 pounds per gallon.. 25 ° 

5. ENDURANCE. 

Hours. 

Full speed (64 gallons gasoline consumption per hour). 7 1 

Cruising speed (44 gallons gasoline consumption per hour). 11^ 

6. WEIGHTS. 

WING STRUCTURE. 

rounds. 

Top planes. 442 

Extensions. 2 ^ 

Center panels. 427 

Lower panels.. 

Vertical stabilizer. ^4 

Horizontal stabilizer. 

Ailerons. 4 ^3 

Nonskid fins. 29 

Rudder. 41 

Tail stays. 07 

Elevators. 00 

Wing floats. 49 2 

Wing fittings and bolts. 154 

Struts. 279 

Wires. 292 


Total wing structure. 2,613 


HULL. 

Shell: 

Sides and fin decking. 166 

Planking. 369 

Steps. 105 

Hood. 121 

Fabric. H 

Sundries. 146 


Shell total. 918 


Skeleton: 

Longerons. 138 

Keel. 47 





































/VOW- WARP / N Q> MATE R/A L. 


FIG. 7.—JIGS OF LEVELING AND ASSEMBLY. 



1 « 4 ; 


90245°—19-2 
































































FIG. 18.—METHOD OF BRACING REAR OF HULL CASE BEFORE 
REMOVING EITHER SIDE OR TOP. THE WEIGHT OF THE HULL 
IS AGAINST THIS SIDE. 



FIG. 19— STENCILING ON SIDE OF HULL CASE. 

































13 


Skeleton—Continued. Pounds. 

Keelson. 51 

Sternpost. 5 

Bracing. 63 

Stringers. 71 

Floors. 97 

Fin timbers and bottom ribs. 89 

Metal fittings. 89 

Stanchions. 132 


Total skeleton weight. 782 


Interior hull accessories: 

Seats. 42 

Hand controls. 61 

Foot controls. 25 

Control wiring. 49 

Flooring. 66 

Bulkheads. 101 

Center bracing (wood)... 28 

Spars.-. 62 

Compression tubes. 14 

Ribs—ends and covering. 82 

Fittings, etc. 45 


Total accessories.-. 575 


Summary of hull weights. 

Shell. 918 

Skeleton. 782 

Interior hull accessories. 575 

Contingency. 56 


Total hull. 2,331 


STEAM ENGINEERING WEIGHTS. 


2 motors, at 882 pounds each. 1, 764 

2 radiators, at 79 pounds each. 158 

. Radiator braces. 6 

Mountings... 258 

Water. 226 

Water piping. 16 











































14 


Pounds. 

2 propellers, at 68 pounds each. 136 

2 windmill gas pumps. 14 

1 hand gas pump. 6 

5 gasoline tanks. 226 

1 gravity tank. 44 

Piping... 35 

2 tachometers and shafting. 22 

2 oil-pressure gauges with piping. 7 

2 water thermometers. 2 

4 oil tanks with piping..:. 81 

4 gasoline gauges. 7 

Liberty tool kit. 31 

2 oil thermometers. 3 

2 hand cranks with gear. 39 

Motor controls. 21 

Ignition wiring. 10 

Contingency.•. 120 


Total. 3,232 


ORDNANCE EQUIPMENT. 

1 Very pistol and ammunition. 15 

1 Lewis gun. 18 

1 shell deflector. 2 

2 Lewis magazines. 20 

1 Scarff ring gun mount. 25 

1 pilot directing bomb sight. 21 

4 bombs, at 230 pounds each. 920 

Bomb gear.. 125 

Installation. 44 


Total. 1 loo 


ELECTRICAL EQUIPMENT. 

Electric lights.*. 12 

Switchboard. 5 

Wiring and installation. 22 

Telephone set. 7 

Range lights. 20 

Signal. 8 


Total.:. 04 














































FIG. 20.—HULL IN CASE READY TO BE BOARDED UP. 























: 

: x.: ; > 


FIG. 21— METHOD OF BRACING HULL IN CASE. BRACES ARE 
2" BY 6" PIECES FASTENED TO DUMMY SIDEWALK BEAMS. 



FIG. 22.—PORT FIN EDGE RESTING IN ITS GROOVE CUT IN THE 

CROSS TIMBER OF THE CASE. 










15 


CONSTRUCTION AND REPAIR EQUIPMENT.. 

Pounds. 

1 sea anchor. 15 

1 bilge pump. 14 

1 air-speed meter. 11 

1 inclinometer. 1 

7 Pyrene fire extinguishers with brackets. 46 

1 bucket. 5 

Radio mast (installed). 15 


Total. 107 


NAVIGATION EQUIPMENT. 

2 compasses. 0 

1 clock.-. 2 

1 altimeter. 

Pigeons. ^ 

Food and water. 30 

Chart board. 4 


Total. 48 


MEDICINE AND SURGERY. 

Medical kit. 10 


RADIO. 

Complete set S. E. 1100, including battery to operate all 

lights, etc. 200 


GASOLINE AND OIL. 

Full oil, 34 gallons, at 7.5 pounds per gallon. 255 

Gasoline, 348 gallons, at 6.25 pounds per gallon. 2,170 

2, 425 


CREW. 

4 men, at 180 pounds each. ^ 2 ^ 









































16 

S'uvxMicLvy . 

Pounds. 

Wing structure. ^13 

Hull......-. 331 

Steam Engineering equipment. 3, 232 

Electrical equipment. 04 

Construction and Repair equipment. 107 

Navigation equipment. 48 

Medicine and Surgery equipment. 1° 

Radio equipment. 260 

Ordnance equipment. R 100 

Crew—4 men. 720 

Gasoline and oil. 2, 425 


Total.-.13,000 
















FIG. 23—HULL FIN EDGE RESTING IN NOTCHED CROSS TIMBER 
OF CASE FRAME HULL BOX IS NOW BUILT AROUND HULL. 



FIG. 24.—THREE-QUARTER VIEW OF HULL 










FIG. 25.—TYPE OF SLIPKNOT USED TO SECURE LIFTING 
ROPES TO SIDEWALK BEAMS. NOTE PADDING UNDER 
ROPE TO PROTECT BEAM FROM CUTTING. 



FIG. 26.—SLING ATTACHED TO REAR ENDS OF DUMMY 
BEAMS IS SECURED TO A TACKLE BLOCK SO THAT 
HULL MAY BE TILTED TO PROPER POSITION FOR 
LOWERING IT INTO CASE. SAME METHOD SHOULD 
BE EMPLOYED FOR LIFTING IT OUT OF THE CASE. 
BRACE BETWEEN BEAMS PREVENTS THEM FROM 
BENDING OUT OF ALIGNMENT. 







PART II 


INSTRUCTIONS FOR ASSEMBLING 


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F-5L FLYING BOAT HANDBOOK. 

INSTRUCTIONS FOR ASSEMBLING. 


1. Shipment. 

A complete boat is packed in eight separate boxes. 

Box No. 1 contains the hull and instruments. 

Box No. 2 contains the engine foundations, radiators 
and oil tanks. 

Box No. 3 contains the main panels. 

Box No. 4 contains the tail units and gravity gasoline 
tank. 

Box No. 5 contains the wing floats. 

Box No. 6 contains the propellers. 

Boxes Nos. 7 and 8 contain the port and starboard 
motors. 

2. Handling Boxes. 

The hull case must be handled with great care to keep 
it in perfect balance. At a point 8 feet from the nose end 
is a notched block; at the end opposite the nose end is 
another such block. These are notched to allow a 1 inch 
cable to rest in them. Two slings should be made, each 
from a piece of cable about 65 feet in length, these being 
ample to pass around the case, resting in the notched 
block and meeting a common tackle block at the top. 
(See fig. 2.) This will insure a balance when lifted. 
The top of each sling should have an eye spliced in the 
cable. The panel and engine boxes may be handled with 
( 19 ) 



20 


any ordinary hoisting equipment and those marked 
“Top” should remain in proper position. 

3. Opening Boxes and Unpacking. 

1. Box No. 1 is the large case containing the hull. 
One side is marked “Open this side.” The roof is first 
removed and then the marked side. Take out all blocks 
and braces and also remove the tail housing. (See fig. 
16.) The tail is in no way attached to the case and is 
easily uncovered. It is important that suitable bracing 
be placed at the side of the case which has not been 
removed, as all the side thrust of the weight of hull is 
against this side. This bracing must be placed before the 
top is removed. 

2. The fuselage covers should be removed before rig¬ 
ging is placed. Care should be taken not to cramp the 
fin "edge when lifting the hull. Sliding or shifting the 
hull laterally must be avoided. 

3. The sidewalk beams are false, being only installed 
for transit. To these, ropes (at least 1 inch in diameter) 
are fastened. (See fig. 24.) A second sling is secured 
to the ends of the two beams against the back side of the 
case and this sling is attached to the center tackle. 

4. Propellers are packed in a separate box. The top 
is fastened by screws. Remove all screws and also the 
nut in the center of lid. The propellers are held in place 
only by the center bolt and are readily lifted out. 

4. Examination of Parts. 

The shipment is made up with a view of compactness, 
and the cases do not necessarily contain complete indi¬ 
vidual units. In each box there is a list of all the parts 
therein. Each part should be carefully examined as it 



FIG. 27.—HULL BEING LIFTED BY A CRANE BLOCK, THE ONE AND 
ONE-HALF INCH ROPES BEING SECURED TO SIDEWALK BEAMS 
NEXT TO HULL SIDES. 

















FIG. 28.—METHOD OF HOLDING THE FOUR ROPES FROM SIDE¬ 
WALK BEAMS TO CENTER LIFTING BLOCK. 




21 


is taken out of its respective box. Any defects should he 
carefully noted so as to be given proper attention and to 
avoid a possibility of being placed on machine. Although 
all parts are thoroughly inspected before being packed, 
they should be again gone over with particular attention 
to the following: 

(a) HULL. 

1. That alignment is correct and no wood members 
are broken. Inspect splices and wrappings. 

2. That bolts are tight and properly cottered. Nuts, 
pins, and cotters, when removed during disassembling, 
are, whenever possible, put back in place. Examine 
threads before tightening nut. Do not force a nut over 
a burred thread. 

3. That wires are taut, free from kinks, and that 
turnbuckles are safety wired. 

4. That instruments are not damaged and wire con¬ 
nections are tight. 

5. That all metal parts are fully covered to protect 
from corrosion. 

6. That gas tank tie downs are secure, safety wired, 
and all lines tight. If a gas line connection is found 
loose, take apart, clean, and put together with a suitable 
sealer. 

( b ) PANELS AND TAIL. 

7. That all surfaces are taut, free from breaks, dents 
and tears. 

8. That no internal parts of panels are broken. It 
being impossible to inspect the interior structure by 
ordinary methods, this part of the work should be passed 
on by an experienced person. 

9. That fittings are tight and properly secured. 

90245°—19-3 


22 


(c) GENERAL. 

10. That all necessary units for completing the as¬ 
sembly are present, and that inclosed lists. check with 
present contents of boxes. 

5. Assembly of Center Section. 

1. Place suitable spreader between upper starboard 
and port longerons to act as support until dummy beams 
have been removed and sidewalk panels attached. 

2. Remove dummy sidewalk beams. Enter sidewalk 
panel beams through sleeve fittings, and place bolts in 
center line and hull side fittings. Remove spreader. 

3. Diagonal braces are strung through fin, bolted to 
fitting at underside of sidewalk panels, and bolted to 
fitting on lower longeron. 

4. Be sure that all nuts are thoroughly secured by 
lock washers. 

5. The spot selected for placing cradle should be com¬ 
paratively level. Two methods of adjusting the cradle 
may be employed: ( a ) placing a screw jack undereach 
corner, or ( b ) using taper wedges which may be driven 
under cradle. 

6. Boat must be leveled both laterally and longitu¬ 
dinally. Level the boat laterally by placing straightedge 
and spirit level across boat on both front and rear 
beams, and jacking up cradle accordingly. Proper level¬ 
ing fore and aft must be taken with respect to the four 
(4) degree angle of attack, measured on underside of side¬ 
walk panels, parallel to center line of hull. A convenient 
method of doing this work is to make a jig as illustrated 
in figure 7, which has two fixed vertical points so arranged 
that when proper angle of incidence is attained bottom 
of jig will be level. A spirit level may either be incor- 



FIG. 29.—PACKING CASE SHOWING ENGINE FOUNDATIONS, RADIA¬ 
TORS, OIL TANKS, AND WATER PIPE MANIFOLDS ATTACHED. 
THIS CASE SHOULDBEKEPTRIGHTSIDEUP, AND IS SO MARKED. 









FIG. 30.—METHOD OF LIFTING CASES, FIG. 31M ETH O D OF LI FT ING PAN ELS OUT 

SHOWING SLINGS PLACED TO INSURE A OF BOX. NOTE THAT SLING IS PLACED 

BALANCE. ONE AND ONE-HALF INCH AROUND PANEL AND SECURED TO 




























23 


porated in, or used in conjunction with, the jig itself. Care 
should he exercised, however, that points of jig he placed 
at all times on center lines of the beams. Should boat he 
moved at any time during process of leveling, it should 
he rechecked for level. Figure 8 shows a jig for longi¬ 
tudinal alignment of hull. 

7. Install two engine section struts at center of boat. 

8. If engines are detached from mountings, they should 
next be installed in same. Radiators may also be 
mounted and water connections secured. 

9. Sufficient supports should now he placed under 
sidewalk beams at hinge points, until engines and wings 
are attached and properly braced by wires. This will 
eliminate warpmg of sidewalk panels due to excessive 
weight. Lift engine mounting (with engine) by means 
of crane or chain falls. If these are not available, motor 
mountings may be skidded into position by use of long 
planks, hut, as this is difficult, it should not be attempted 
unless absolutely necessary. Connect up diagonal braces 
from engine mountings to fittings on center of sidewalk 
beams. Connect up ail stays and wires and adjust 
these to a fair tension. Engine beds should be level 
both laterally and longitudinally when boat is level. 

10. Connect all piping and electrical wiring to engine. 

11. Raise engine section panel into place, attach struts 
and wires and connect up gasoline piping to gravity tank. 

12. Check level of engine section panel by placing 
straightedge with spirit level along front and rear beams, 
or by measuring distance between upper and lower hinge 
both front and rear. 

13. Check for zero (0) degree stagger by dropping 
plumb line over leading edge at both outer ends of up¬ 
per engine section panel. Adjust stagger wires to bring 


24 


leading edge of upper panel directly over leading edge 
of sidewalk panels. 

6. Assembly of Outer Wing Panels. 

1. Connect upper intermediate and upper outer panels 
at hinges (without ailerons). Stand upper and lower 
wing panels on their leading edge parallel to each other. 
Connect panels with struts and stay wires. Interplane 
struts are numbered as per diagram, figure 10. Tighten 
wires to approximately flying tension. 

2. Attach nonskid fins and supporting wires, and see 
that top beam is in alignment and nonskid fins normal. 

3. Do not tighten flying wires to overhang excessively 
or too much tension will be thrown on upper king-post 
brace wires. 

4. Raise assembled panels, engage two hinges on lower 
panel and hinges on sidewalk, enter hinge pins, and then 
raise panel assembly at outer end and connect up the 
two upper hinges of intermediate panel with hinges on 
engine section panel. Support assembly until landing 
wires are fastened. (See fig. 4.) Unless panel assem¬ 
blies on starboard and port sides are raised into place 
simultaneously, supports under one side must not be 
removed until opposite side has been assembled and wires 
fastened. 

5. As an alternate method of erecting panels, connect 
upper intermediate and upper outer panels at hinge 
points, attach nonskid fins and upper brace wires to 
same. Raise this assembly into place ,by use of slings 
(fig. 3), which remain in place until erection is completed. 
Connect up interplane struts and brace wires at strut 
fittings of upper panel. Attach lower panel at sidewalk 
hinges and connect struts to wires. After wires are made 



FIG. 32.—DETACHABLE SIDEWALK PANEL PARTLY REMOVED. 

LOOKING FORWARD. 



FIG. 33.—SPLICE IN SIDEWALK BEAM WITH STARBOARD PIECE 

PARTLY REMOVED. 







FIG. 34.—SIDEWALK PANEL REMOVED AFTER FITTING AND READ 
FOR UNDERSIDE COVERING. PORT PANEL TO BE MARKE 
“P” AND STARBOARD PANEL “S,” WITH BOAT NUMBER FOL 
LOWING LETTER. TOP SURFACE OF THESE PANELS IS COVERE 
WITH VENEER. 














25 


fast, overhead slings can be removed. After erection 
by either first or second method, proceed as follows: 

6. Attach ailerons and secure hinge pins. While this 
can be done on the ground it is advisable to assemble 
them after panel erection, owing to their size and weight. 

7. Connect up all control wires to ailerons, adjusting 
lengths of wires to obtain a continuation of the lines of 
the panel. 

8. Adjust landing wires so as to get proper alignment 
of wings and approximately correct tension. Tighten 
flying wires, giving these slightly less tension than landing 
wires. 

9. Adjust stagger wires, giving each of these equal 
tension. 

10. Sight along leading and trailing edges of upper and 
lower panels, from center, and see that edges are straight 
and parallel to each other, and that ailerons are in line 
with wings. 

11. Check for zero (0) degree stagger by use of a series 
of plumb bobs dropped from leading edge of upper 
wings. 

12. Angle of incidence of four (4) degrees can be 
checked with same gauge as used on sidewalks when level¬ 
ing up boat. Check between beam centers at several 
points along wing, so as to detect any warp. 

13. Dihedral angle of one and a half (1^) degree can 
be determined by use of a long straightedge equipped 
with a protractor level or a straightedge planed to the 
required angle and using a spirit level on top edge. 
(See figs. 5 and 6.) 

14. With struts in position and a zero (0) degree 
stagger, the angle of incidence of top plane can be 
checked by measuring the gap between upper and 


26 


lower leading edges and upper and lower trailing edges, 
providing the lower panel has been properly set at the 
required angle. Distance is 8 feet 10}/2 inches. 

15. See that all control wires to ailerons have the same 
tension. 

16. Attach pontoons to lower wing panel tips. 

17. Fasten bomb-dropping devices, and see that 
U bolts are not set up tighter than necessary to secure 
them. 

18. Check up length of drift wires from each side of 
nose to upper and lower wing panels. Have these wires 
of equal length and tension. This will square wings 
with axis of hull. Follow same procedure with brace 
wires from horizontal stabilizer to square stabilizer with 
hull. 

19. Inspect all wires, clevises, cotter pins, turnbuckles, 
pipe lines, wiring, controls, tie-rods and connections 
throughout boat, and see that everything is taut and in 
proper shape. Place safety wires on all turnbuckles 
after their final adjustment. Turnbuckles should not 
show over three threads outside of barrel, or less than 
% inch of shank when they are finally adjusted. 

20. Attach propellers, guns, and all accessories. 

7. Assembly of Tail Surfaces. 

1. Tail surfaces can be assembled at any time after 
hull has been leveled. 

2. Attach fin and check so that fin is exactly vertical 
when boat is level. 

3. Set horizontal stabilizer over fin and fasten to fin 
by vertical tie-down bolt in front and by metal clip on 
rear. 



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FIG. 35.—TH REE-QUARTER VIEW OF CRADLE USED FOR HOLDING 
HULL DURING ASSEMBLY. BED IS SHAPED TO FIT HULL BOT¬ 
TOM WITH STEP, AND PADDED WITH ONE-INCH SOFT FELT. 
CASTORS AT EACH CORNER FACILITATE SHIFTING OF HULL. 
USUAL METHODS OF LEVELING MAY BE EMPLOYED AFTER 
CRADLE IS PLACED IN POSITION. 



FIG. 36.—THROTTLE CONTROLS FOR MOTORS. NOTE DOWN POSI¬ 
TION OF PORT SEAT. STARBOARD SEAT IS STATIONARY. 








FIG. 37—INSTRUMENT BOARD WITH NEW TYPE BOMB SIGNAL 

DISK AT RIGHT END. 



FIG. 38—RUDDER CONTROL LOOKING AFT. 











27 


4. Attach all forward steel stabilizer braces and 

T tS1 ijV e f r braces > and set a]1 stay wires. Stabilizer 
should be level laterally when hull is level. 

5. Horizontal stabilizer is set with a two and one-half 
(2M) degrees angle of incidence, and a straight line drawn 
through leading and trailing edges should be at an amde 
oi two and one-half (2}4) degrees with engine beds. 
Check this angle by using jig (fig. 7) along top of stabilizer 
from front to rear beam, parallel to hull. Check this 
angle near fin and again at outer ends of stabilizer to 
see that there is no warp. 

6. Attach rudder and secure hinge pins. Fasten 
l udder balance panel to rudder and connect up remain¬ 
ing two steel braces to stabilizer. Attach elevators 
at hinge points and secure with locking pins. Smaller 
horns are attached to underside of elevators. Stay 
wires from control horns on ailerons and elevators to 
trailing edges may be used to straighten out warp in 
these surfaces. Control wires on elevators should be 
adjusted so that when control column is in neutral 
position, elevators will be at the same angle of incidence 
as the horizontal stabilizer. Control wires should be 
allowed a little slack in their neutral position to avoid 
binding in extreme positions. Rudder-control wires 
should be fairly taut but should not cause binding on 
rudder pins. 


8. General Information. 

PIPE LINES. 

The fuel lines are shown in figure 15. They are all 
marked with a red band painted on each end so as to be 
easily distinguished from other piping. 


28 


The air lines, including vents from fuel tanks and air 
speed meter, are marked with a blue band. 

The tube leading to the oil-pressure gauges on the in¬ 
strument board is marked with a white band. 

The water pipes are marked with a yellow band and 
compressed air or starter pipes are marked with black 
bands. 

The brass tubing on both port and starboard side con¬ 
tains the bomb release control wires. These have no 
mark on them. 

HAND PUMPS. 

There are two hand pumps of similar construction, 
one for pumping fuel into the gravity tank for starting 
and emergency and the other for pumping bilge. These 
pumps are of the semi-rotary type and are easily taken 
apart for inspection and repair. The fuel pump is 
located on the after center stanchion, and the bilge pump 
aft of the forward center stanchion. 

LUBRICATION. 

Figures 11 and 12 show points on boat which require 
lubrication of grease and oil aside from motors. These 
charts show all ferrules and pulleys which will need at¬ 
tention to prevent undue wear and aid in easy control 
of the moving parts. 



FIG. 39.—INSTRUMENT BOARD WITH PORT PILOT’S TELEPHONE STATION AT LEFT SIDE. 














FIG. 40.—INTERIOR VIEW OF FORWARD GUNNER’S PIT. ON PORT 
SIDE IS SHOWN HEATING CONNECTION AND SWITCH. NOTE 
TRIGGERS FOR CONTROL OF BOMB RELEASE. INSTRUMENT IS 
AN ALTIMETER. 



FIG. 41 .—INSTRUMENT BOARD. BOMB SIGHT DIAL (OLD TYPE) 
IS ON STARBOARD AVIATOR’S SIDE. COMPASS IS ON PORT 
SIDE. 













PART III 


PACKING SHEETS 


902 45 0 — 19=—4 


( 29 ) 















- 








•».* 












* 




.* 





























. 






Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

INDEX SHEET. 

Boat No. 

9 Packing Sheets. 

8 Boxes. 

Sheet No. 1 and 2 (Box No. 1), Hull. 

Sheet No. 3 and 4 (Box No. 1), Instruments. 

Sheet No. 5 (Boxes Nos. 2 and 6), Engine Foundations and 
Propellers. 

Sheet No. 6 (Box No. 3), Main Panels. 

Sheet No. 7 (Box No. 4), Tail Units. 

Sheet No. 8 (Box No. 5), Wing Floats. 

Sheet No. 9 (Boxes No. 7 and 8), Motors. 

Date. Time. 

Left factory for yard: 

Box No. 1,. 

Box No. 2,. 

Box No. 3,. 

Box No. 4,. 

Box No. 5,. 

Box No. 6,.-. 

Box No. 7,.. 

Box No. 8,.•. 


Inspector, 

(311 


THIS IS 



FOR Or F1CIAL USE . ONLY 

ACCOUNTED FOB IN ACCORDANCE With PAR. 693 A. 




















32 


Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

HULL. 

Boat No. Sheet No. 1 

Box No. 1. 

Port Side, Stern to Bow. 

1 boat hull, complete, with 1 lower tail clip, 1 upper tail clip. 

4 horizontal stabilizer drift wires with 4 tumbuckles, 4 shackles 
with clevis pins. 

4 horizontal stabilizer brace wire with 4 tumbuckles, 4 eye bolts 
with nuts. 

2 horizontal stabilizer brace sockets with 2 bolts, nuts and lock 

washers. 

1 horizontal brace-wire clip. 

1 sidewalk brace wire clip, turnbuckle attached. 

1 access door. 

1 coil of -iVinch flexible cable for bomb release. 

4 sidewalk supporting bolts with nuts and lock washers. 

1 pilot step. 

1 rope cleat. 

Bow. 

1 right and 1 left drift wire clip with 4 drift wires with 4 tumbuckles 
attached and 1 end of each wire open, 8 thimbles, 8 shackles 
with clevis pins, 2 triple connecting plates, 2 aileron control 
wires; 2 long and 2 short tie wires. 

1 towing cable with rope attached leading through fitting in bow. 

1 tow plate. 

Starboard Side, Bow to Stern. 

1 pilot step. 

1 coil of -j^-inch flexible cable for bomb release. 

4 sidewalk supporting bolts with nuts and lock washers 
1 sidewalk brace wire clip with turnbuckle attached. 

1 access door. 

1 brace wire clip. 

2 horizontal stabilizer brace sockets with 2 bolts, nuts and lock 

washer. 

Shortage. 

Remarks... 


Inspector 







LU O 
cr — 

< o 

< 
c/) cr 

LLl 

i o- 

O 2 

t -l 

^O 

x DC of 

h- O o 
O p 
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Oujo 

o i_ o 

^ < Q 

I 2 < 
h O 01 
O j~ cr 
m ^O 
H m u - 

O □ 2 
2 0 
{2 2» H- 

t; o o 

cr LU 

O 2 

5^0 

t I o 

£ o o 

(/) _J 3 
LU ’ LLl CL 

“* C5 _ 
7 CD 
Z 

h- 
< 
LU 

I 


o 

CL 

i 

cr 

Z) 

O 

LL 


< 

cr 

□ 


h- cr 
° z 
cr u ^ 


< 

O 

CO 

cr 
< 
l— 
c r > 


CN 


CD 

ll 


< 

D . 
cr rr 
I— O 

</> b- 
z < 

~ cr 
cr LU 

° 2; 

Ll O 



















FIG. 43.—LOOKING AFT OVER FUEL TANKS. 

























Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

EQUIPMENT ASSEMBLED INSIDE OF HULL. 

Boat No. Sheet No. 2. 

Box No. 1. 

1 bomb release with 6 pulleys, 8 flexible cables leading through 
tubing to port and starboard side. 

1 Davis gun mount. 

1 cleat. 

8 ammunition trays. 

1 generator box. 

2 generator regulators. 

2 rudder foot bars with 4 stirrups, 1 Sandow clip, 2 adjustable cable 
terminals and 4 control wires with turnbuckles, shackles and 
clevis pins. 

1 rudder Sandow and 1 elevator Sandow. 

2 Liberty switches. 

2 pilots’ seats with cushions. 

1 double aileron and elevator control device complete with 1 check 

wire, 4 elevator control wires, 2 aileron control wires. 

2 wind shields. 

2 spark controls with 4 cables and 4 turnbuckles. 

2 throttle controls with 4 cables and 4 turnbuckles. 

1 battery box in fin recess on port side. 

2 storage batteries. 

5 gasoline tanks, each equipped with filler, cap and gauge, and 1 

with flow sight box. 

6 Pyrene fire extinguishers with brackets. 

2 out-rigger gun mounts. 

1 sliding door over rear gunner’s cockpit. 

1 bilge pump with hose. 

1 windmill pump with all connections. 

1 gasoline hand pump. 

2 sidewalks. 

4 sidewalk braces. 

4 English bomb gears complete. 

Very pistol cartridge rack. 

Shortages. 

Remarks. 

Reed, from final assembly 

Date packed. 

Packed by. 

Weight, net. 

Weight, gross. 


Checked by 
Inspector .. 












Naval Aircraft Factory. 


Packing List for F-oL Boat Seaplane. 

INSTRUMENTS. 

Boat No. Sheet No. 3. 

Box No. 1. 

1 safety belt in forward gunner’s cockpit. 

1 Scarff ring gun mount in forward cockpit. 

1 Scarff ring gun mount in after cockpit. 

1 vertical compass, No., Navy Standard I. 

1 flat compass with two electric bulbs, No. 

1 combination inclinometer, No. 

2 oil pressure gauges, Nos. 

2 tachometers, Nos. 

1 airspeed meter, No. 

1 radio clock, No. 

2 altimeters, Nos. 

1 four pole, one-way switch on starboard side. 

2 dash light push button switches on starboard side. 

2 dash lights on instrument board. 

1 name plate. 

1 airspeed meter horn with coil of |-inch copper tubing. 

3 wiring diagrams; ignition, telephone, heating and lighting. 

1 bomb sight telltale on instrument board. 

1 bomb sight Mark V, No. 

1 bomb sight fixture on bow. 

2 oil thermometers, Nos. 

2 water thermometers, Nos. 

3 spare 15-foot thermometer tubes, Nos.. 

1 spare 18-foot thermometer tube, No. 

Spare parts as per specification PSP-7. 

1 package of construction blue prints for assembly of boat, drawings 
Nos. 41102, 5412, 5414, 6326, 6327, 6323, 6332, 6833, 5834, 5835, 
and 6836. 

Shortage. 

Remarks. 




















FIG. 


44.—THREE-QUARTER 
TANKS AND LOWER 


VIEW LOOKING AFT OVER GASOLINE 
PIPING. READY FOR SHIPMENT. 





































FIG. 45—GASOLINE MANIFOLD SHOWING CUT-OFF VALVES TO 
VARIOUS TANKS AND WIND PUMP. 



FIG. 46.—AFTER COCKPIT. TELEPHONE STATION IS LOCATED 
ON STARBOARD SIDE OF HULL JUST FORWARD OF'ACCESS 
DOOR. HEATING CONNECTION IS SHOWN ATTACHED TO 
CENTER STANCHION. ON FORWARD SIDE OF STANCHION IS 
HAND GASOLINE PUMP. 










Naval Aircraft Factory. 


Packing List for F—5L Boat Seaplane. 
instruments—( continued.) 

Boat No. 

1 telephone outfit, complete: 

4 standard station boxes. 

Cable. 

1 radio operator’s station box. 

1 battery and container assembled in hull. 

1 extra battery. 

4 mouthpieces. 

4 telephone headgear sets. 

1 radio outfit, complete: 

1 radio transmitter outfit. 

1 receiver, No. 

3 vacuum tubes. 

1 collapsible mast. 

1 24-volt storage battery. 

1 antenna system, No. 

1 generator, No. 

1 box spare parts, No. 

1 radio compass. 

1 heating and lighting outfit, complete: 

Interior hull wiring. 

1 green running light. 

1 red running light. 

1 white range light. 

Outside wiring. 

Shortages. 

Remarks. 

Checked by. 

Inspector. 


Sheet No. 4. 
Box No. 1. 









36 


Naval Aircraft Factory. 
Packing List for F-5L Boat Seaplane. 


Sheet No. 5. 
Box No. 2. 

Boat No. .. Box No. 6. 

ENGINE FOUNDATIONS WITH EQUIPMENT, BOX NO. 2. 

1 port and 1 starboard engine foundation with 8 y\ braces and 8 V struts. 
8 cables with turnbuckles, shackles and clevis pins. 

4 pulleys. 

2 split brass bushings for starter. 

2 distributor arms and 2 connecting rods. 

1 port radiator, No., with 2 wires and 2 braces. 

1 starboard radiator, No., with 2 wires and 2 braces. 

4 oil tanks with 12 clamps and 4 pieces of -J-inch copper tubing. 

90 hose clamps. 

2 large water pipes with 2 plugs and 6 hose connections. 

4 water pipe brackets. 

28 engine bed bolts. 

4 T oil lines with 12 hose connections. 

2 priming pumps. 

Shortages. 

Remarks. 

Weight. 

Date packed. 

Packed by. 

Inspector. 

PROPELLERS, BOX NO. G. 


8 propellers, Nos 

Weight... 

Date packed. 

Packed by.. 


Inspector 

















TELEPHONE SYSTEM. 








» 


FIG. 48—TAIL BRACE ASSEMBLY. 


























37 


Naval Aircraft Factory. 


Packing List for F-5L Boat Seaplane. 


Boat No 


MAIN PANEL BOX. 

Sheet No. 6. 
Box No. 3. 


1 right and 1 left intermediate panel, each with 4 hinge pins in 
female hinges, 4 male hinges, G post sockets with bolts, nuts, 
and cotters, 2 aileron control wires and 23 cables with turn- 
buckles attached. 

1 right and 1 left lower panel each with 6 post sockets, bolts, nuts 

and cotters, 4 male hinges and 4 sets of English bomb clips. 

2 nonskids, 1 right and 1 left, each with 6 cables and turnbuckles. 

1 right and 1 left aileron with 10 hinge pins in female hinges; 10 

bolts, nuts, and cotters. 

12 interplane struts numbered from 1 to 12. 

1 right and 1 left upper outer panel each with 14 male hinges, 4 
cables with turnbuckles attached and 4 V-bolts with pulleys 
attached. 

8 ailerons, horns with wires, bolts and nuts. 

Shortage. 

Remarks. 

Weight. 

Bate packed. 

Packed by. 

Checked by. 

Inspector. 










38 


Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

TAIL UNIT BOX-. 

Sheet No. 7. 
Box No. 4 

Boat No. 

1 engine section panel with gravity tank, 8 hinge pins in female, 
hinges, 6 post sockets with bolts, nuts, and cotters; 30 cables 
with turnbuckles attached, and 4 pulleys. 

1 horizontal stabilizer with 8 brace fittings, 10 hinge pins in female 

hinges and 10 bolts, nuts and cotters, 4 wire guides. 

2 elevators each equipped with 5 male hinges, 5 bolts, nuts and 

cotters. 

1 rudder balance with 2 wires and fittings. 

1 rudder with 7 female hinges. 

1 vertical stabilizer with 7 male hinges with hinge pins and 1 hori¬ 

zontal stabilizer brace fitting. 

4 rudder horns. 

8 elevator horns. 

8 horizontal stabilizer braces with fittings. 

4 diagonal braces with ignition wires and guides. 

2 gasoline lines. 

2 center section struts with gasoline lines attached. 

Shortage. 

Remarks. 

Weight... 

Date packed. 

Packed by. 

Checked by.. .. 

Inspector..... 













FIG. 49.—SIDE VIEW OF 


NEW TYPE BOMB SIGFIT ATTACHED 
TO BOW. 


90245°—19' 


■5 









FIG. 50.—TOP VIEW OF NEW 

ro 


TYPE 

BOW. 


BOMB SIGHT 


ATTACHED 




































39 


Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

WING FLOATS. 

Boat No. Sheet No. 8. 

Box No. 5. 

2 wing floats with 8 fittings. 

8 washer plates. 

8 wooden blocks. 

16 bolts, nuts, cotters, and flat and bevel washers. 

Shortage. 

Remarks. 

Weight. 

Date packed. 

Packed by. 

Checked by. 

Inspector. 










40 


Naval Aircraft Factory. 

Packing List for F-5L Boat Seaplane. 

Sheet No. 9. 

Boat No. Box No. 7. 

Box No. 8. 

PORT MOTOR, BOX NO. 7. 

1 Port motor, Navy No.Maker.Starter, No. 

1 fair lead with bracket. 

1 gas strainer with 2 pipe connections. 

1 carburetor control rod with pulley. 

1 carburetor overflow pipe. 

1 oil line. 

1 motor cover. 

1 log book. 

1 kit of tools. 

1 box of spare motor parts. 

1 primer. 

1 propeller hub. 

Shortage. 

Remarks. 

Weight... 

Date packed.... 

Packed by. 

Inspector. . 

STARBOARD MOTOR, BOX NO. 8. 

1 Starboard motor, Navy No.Maker. Starter, No. 

1 fair lead with bracket. 

1 gas strainer with 2 pipe connections. 

1 carburetor control rod with pulley. 

1 carburetor overflow pipe. 

1 oil line. 

1 motor cover. 

1 log book. 

1 kit of tools. 

1 box of spare motor parts. 

1 primer. 

1 propeller hub. 

Shortage. 

Remarks. 

Weight. 

Date packed. 

Packed by. 


Inspector 






















FIG. 51a—REAR VIEW OF BOW FIG. 51b.—FRONT VIEW OF BOW 
GUN MOUNT. GUN MOUNT. 



FIG. 52.—REAR GUN MOUNT, HATCH COVER CLOSED. 






















FIG. 53a—VIEW OF MOTOR WITH OIL AND WATER PIPING. LOOKING 

FORWARD 



FIG. 53b.—VIEW OF MOTOR FROM UNDERNEATH. LOOKING AFT. 







PART IV 


TABLES 


( 41 ) 





















* 









































f 

« 












































t 


























V 







Table No.' 1. —Specific gravity equivalents for degrees Baume for liquids 

lighter than water. ‘ 


Formula; Degrees Baume =-= 130 

60° 

Sp. gr. - F. 

60° 

[Sp. gr. taken at 60° F. and referred to distilled water at 60° F.] 


Baume. 

Specific 

gravity. 

Pounds 

per 

gallon. 

Baume. 

Specific 

gravity. 

Pounds 

per 

gallon. 

Baum6. 

Specific 

gravity. 

Pounds 

per 

gallon. 

10 

1.0000 

8.33 

37 

0.8383 

•6.98 

64 

0.7217 

6.01 

11 

. 9929 

8.27 

38 

.8333 

6.94 

65 

.7179 

5.98 

12 

.9859 

8.21 

39 

.8285 

6.90 

68 

.7143 

5.95 

13 

.9790 

8.16 

40 

.8235 

6.86 

67 

.7107 

5.92 

11 

.9722 

8.10 

41 

.8187 

6.82 

68 

.7071 

5.89 

15 

.9655 

8.04 

42 

.8139 

6.78 

69 

.7035 

5.86 

16 

.9589 

7.99 

43 

.8092 

6.74 

70 

.7000 

5.83 

17 

.9524 

7.93 

44 

.8046 

6. 70 

71 

.6965 

5.80 

18 

.9459 

7.88 

45 

.8000 

6.66 

72 

.6931 

5.78 

19 

.9396 

7.83 

46 

.7955 

6.63 

73 

.6897 

5.75 

20 

.9333 

7.78 

47 

.7909 

6.59 

74 

.6863 

5.72 

21 

.9272 

7.72 

48 

.7865 

6.55 

75 

. 6829 

5.69 

22 

.9211 

7.67 

49 

.7821 

6.52 

76 

.6796 

5.66 

23 

.9150 

7.62 

50 

.7777 

6.48 

77 

.6763 

5.63 

21 

.9091 

7.57 

51 

.7735 

6.44 

78 

.6730 

5.60 

25 

.9032 

7.53 

52 

. 7692 

6.41 

79 

.6698 

5.58 

26 

.8974 

7.48 

53 

.7650 

6.37 

80 

.6666 

5.55 

27 

.8917 

7.43 

54 

.7609 

6.34 

81 

.6635 

5.52 

28 

.8861 

7.38 

55 

.7568 

6.30 

82 

.6604 

5.50 

29 

.8805 

7.34 

56 

.7527 

6.27 

83 

.6573 

5.48 

30 

.8750 

7.29 

57 

.7487 

6.24 

84 

. 6542 

5.45 

31 

.8696 

7.24 

58 

.7447 

6.20 

85 

.6511 

5.42 

32 

.8642 

7.20 

59 

.7407 

6.17 

86 

.6481 

5.40 

33 

.8589 

7.15 

60 

.7368 

6.14 

87 

.6451 

5.38 

31 

.8537 

7.11 

61 

.7329 

6.11 

88 

.6422 

5.36 

35 

.8485 

7.07 

62 

.7292 

6.07 

89 

.6392 

5.33 

36 

.8433 

7.03 

63 

.7254 

6.04 

90 

.6363 

5.30 











( 43 ) 




























44 


Table No. II.— Metric conversion table. 


[English to Metric.] 


English 

units. 

Hundredths 
of an inch to 
millimeters. 

Feet to 
meters. 

Miles to 
kilometers. 

Gallons to 
liters. 

Pounds to 
kilograms. 

1. 

0.254 

0.30480 

1.6093 

3. 7853 

0.45359 

2. 

.508 

.60960 

3.2187 

7. 5707 

. 90718 

3. 

. 762 

.91410 

4.8280 

11.3560 

1.36078 

4..... 

1.016 

1.21920 

6.4374 

15.1413 

1.81437 

5. 

1.270 

1.52400 

8.0467 

18.9267 

2. 26796 

6. 

1.524 

1.83830 

9.6561 

22. 7120 

2.72155 

1 . 

1.778 

2.13360 

11.2654 

26.4973 

3.17515 

8. 

2.032 

2.43840 

12.8748 

30.2827 

3. 62874 

9. 

2.286 

2.74321 

14.4841 

34.0680 

4.03233 

10. 

2.540 

3.04801 

16.0935 

37.8533 

4.53592 

11. 

2. 794 

3.35281 

17. 7028 

41.6387 

4.93552 

12. 

3.048 

3.65761 

19.3122 

45. 4240 

5.44311 

13. 

3.302 

3.96241 

20.9215 

49.2093 

5.89670 

14. 

3. 556 

4.26721 

22.5309 

52. 9947 

6.35029 


3.810 

4.57201 

21.1402 

56.7800 

6.80389 

16. 

4. 064 

4.87681 

25. 7496 

60. 5653 

7.25743 

17. 

4.318 

5.18161 

27.3589 

64. 3506 

7. 71107 

18. 

4. 572 

5.48641 

28.9682 

68.1360 

8.16466 

19. .... 

4.826 

5. 79121 

30. 5776 

71.9213 

S. 61826 

20. 

5.0-10 

6. 09601 

32.1869 

75. 7086 

9.07185 

21. 

5. 334 

6.40081 

33. 7963 

79.4920 

9. 52544 

22. 

5.58S 

6. 70561 

35.4056 

83. 2773 

9.97903 

23. 

5.842 

7.01041 

37. 0150 

87.0626 

10. 43263 

24. 

6.096 

7.31521 

38.6243 

90. 8480 

10.88622 

25. 

6.350 

7.62002 

40.2337 

94.6333 

11.33981 

26. 

6. 604 

7.92482 

41.8430 

98. 41S6 

11.79340 

27. 

6.858 

8.22962 

43.4524 

102. 2040 

12.24700 

28 . 

7.112 

8. 53442 

45.0817 

105.9893 

12. 70059 

29. 

7.336 

8.83922 

46. 6711 

109. 7746 

13.15418 

30. 

7. 620 

9.14402 

48.2804 

113.5600 

13.60777 

31.. 

7.874 

9.448S2 

49. 8898 

117.3453 

14. 06137 

32. 

8.128 

9. 75362 

51.4991 

121.1306 

14.51496 

33. 

8.382 

10.05842 

53.1035 

124.9160 

14.96855 

34. 

8. 636 

10. 36322 

54.7178 

128. 7013 

15.42214 

35. 

8.890 

10. 66802 

56. 3272 

132.4866 

15.87573 

35. 

9.144 

10.97282 

57.9365 

136.2720 

16.32933 

37. 

9.398 

11.27762 

59. 5458 

140. 0573 

16. 78292 

38. 

9.652 

11.58242 

61.1552 

143.8426 

17. 23651 

39. 

9.906 

11.88722 

62. 7645 

147.6280 

17.69010 

40... 

10.160 

12.19202 

64. 3739 

151.4133 

18.14370 

41. 

10.414 

12.49682 

65.9332 

155.1986 

18.59729 

42. 

10. 668 

12. 80163 

67. 5926 

158.9340 

19. 05088 

43. 

10. 922 

13.10643 

69. 2019 

162. 7693 

19.50447 

44. 

11.176 

13.41123 

70. 8113 

166. 5516 

19. 95807 

45. 

11.430 

13.71603 

72. 4206 

170. 3400 

20.41166 

46. 

11.684 

14. 02083 

74.0300 

174.1253 

20. 86525 

47. 

11.938 

14.32563 

75.6393 

177.9106 

21.31880 

48. 

12.192 

14.63043 

77. 2487 

181.6960 

21.77244 

49. 

12.446 

11.93523 

78. 8580 

185.4813 

22. 22603 

50. 

12. 700 

15. 24003 

80. 4674 

189.2666 

22. 67962 

100. 

25.400 

30.48006 

160.9347 

378.53 0 

45.35924 












































































FIG. 54. —TH REE-QUARTER REAR VIEW OF CENTER SECTION. 



















































FIG. 55.—FRONT VIEW OF COMPLETE ASSEMBLY. 


































Table No. III .—Metric conversion table. 

[Metric to English.] 


Millimeters 
to inches. 

Meters to 
feet. 

Kilometers 
to miles. 

Liters to 
gallons. 

Kilograms 
to pounds. 

0.03937 

3.28083 

0.62137 

0.26418 

2.2046 

.07874 

6.56167 

1.24274 

.52836 

4.4092 

.11811 

9. 84250 

1.86411 

.79253 

6. 6139 

. 1.5748 

13.12333 

2.48548 

1.05671 

8. 8185 

. 19685 

16. 40417 

3.10685 

1.32089 

11.0231 

.23622 

19. 68500 

3. 72822 

1.58507 

13.2277 

.27559 

22.96583 

4.34959 

1.84924 

15.4324 

.31496 

26.24667 

4.97096 

2.11342 

17.6370 

.35433 

29. 52750 

5.59233 

2.37760 

19.8416 

.39370 

32. 80833 

6.21370 

2. 64178 

22.0462 

.43307 

36.08917 

6.83507 

2.90595 

24.2508 

.47244 

39. 37000 

7.45644 

3.17013 

26.4555 

.51181 

42. 65083 

8.07781 

3.43431 

28. 6601 

.55118 

45.93167 

8.69918 

3. 69849 

30.8647 

.59055 

49.21250 

9.32055 

3. 96266 

33.0693 

.62992 

52.49333 

9.94192 

4.22684 

35.2740 

.66929 

55. 77417 

10. 56329 

4.49102 

37.4786 

.70866 

59. 05500 

11.18466 

4. 75520 

39. 6832 

.74803 

62.33583 

11.80603 

5.01937 

41.8878 

.78740 

65. 61667 

12.42740 

5.28355 

44. 0924 

.82677 

68.89750 

13.04877 

5.54773 

46.2971 

.86614 

72.17833 

13.67014 

5. 81191 

48.5017 

. 90551 

75.45917 

14.29151 

6.07608 

50. 7063 

. 94488 

78. 74000 

14.91288 

6. 34026 

52. 9109 

.98425 

82.02083 

15.53425 

6.60444 

55.1156 

1.02362 

85.30167 

16.15562 

6. 86862 

57.3202 

1.06299 

88.58250 

16. 77699 

7.13280 

59. 5248 

1.10236 

91.86333 

17.39836 

7.39697 

■61.7294 

1.14173 

95.14417 

18.01973 

7.66115 

63. 9340 

1.18110 

98. 42500 

IS. 64110 

.7.92533 

66.1387 

1.22047 

101.70583 

19.26247 

8.18951 

68.3433 

1.25984 

104.98667 

19. 88384 

8. 45368 

70. 5479 

1.29921 

108. 26750 

20.50521 

8.71786 

72. 7525 

1.33858 

111.54833 

21.12658 

8.98204 

74. 9572 

1.37795 

114.82917 

21.74795 

9.24622 

77.1618 

1.41732 

118.11000 

22.36932 

9. 51039 

79.3664 

1.45669 

121.39083 

22.99069 

9. 77457 

81.5710 

1.49606 

124. 67167 

23. 61206 

10.03875 

83. 7756 

1.53543 

127.95250 

24.23343 

10.30293 

85.9803 

1.57480 

131.23330 

24.85480 

10. 56710 

88.1849 

1.61417 

134. 51417 

25.47617 

10.83128 

90.3895 

1.65354 

137. 79500 

26.09751 

11.09546 

92.5941 

1.69291 

141.07583 

26. 71891 

11.35964 

94. 7988 

1.73228 

144.35667 

27.34028 

11.62381 

97.0034 

1.77165 

147.63750 

27.96165 

11.88799 

99.2080 

1.81102 

150.91833 

28. 58302 

12.15217 

101.4126 

1.85039 

154.19917 

29.20439 

12. 41635 

103.6173 

1.88976 

157. 48000 

29. 82576 

12.68052 

105.8219 

1.92913 

160. 76083 

30. 44713 

12.94470 

108.0265 

1.96850 

164.04167 

31.06850 

13. 20888 

110.2311 

3. 93700 

328.08334 

62.13700 

26.41776 

220.4622 





































































46 


Table No. IV. — Variation of wind velocity with altitude during the day. 


Elevation. 


Velocities in miles per hour. 


Surface . 

5 

10 

15 

20 

25 

500 feet. . 

7 

15 

21 

28 

35 

1 000 feet . 

8 

18 

26 

34 

43 

2 000 feet . 

8 

18 

28 

37 

47 

3 ’ 000 feet . 

8 

18 

29 

40 

49 

\ 000 feet . 

10 

19 

29 

40 

50 

5 000 feet. 

13 

20 

29 

40 

50 








Table No. IV. — Variation of direction of wind and altitude. 

[Upper-region winds vary in direction from those near the earth’s surface. The 
amount of deviation is given approximately in the tabulation.] 


Elevation. 

Devia¬ 
tion to . 
right in 
degrees. 

Directions. 

Surface_ 

0 

N. 

E. 

S. 

w. 

500 feet. 

1,000 feet. 

5 

10 

N.1E. 

N. by E. 

E. 1 S. 

E. by S. 

S. 1 w. 

S. by W. 

W. 1 N. 

W. bv N. 

2,000 feet... 

16 

N. by E.iE.. 

E. by S. JS... 

S. by W. i W. 

W. by N. 1 N. 

3,000 feet... 

19 

N. by E.f E.. 

E. bv S. fS... 

S. bv W. | W. 

W. bv N. J N. 

4,000 feet 

20 

NNE. 

ESE. 

ssw . 

WNW. 

5,000 feet... 

21 

NNE. 

ESE. 

ssw . 

WNW. 

























































FIG. 56. —STAGING FOR WING ASSEMBLY. 




















































































































47 


Table VI .—Compass points and their equivalents. 


o r 

Points. 

O 

/ 

Points. 

o / 

Points. 

O / 

Points 

0 00 

N 

90 

00 

E 

180 00 

S 

270 00 

W 

2 49 

N i E 

92 

49 

E i S 

182 49 

SAW 

272 49 

WJN 

5 38 

N IE 

95 

38 

E as 

185 38 

SAW 

275 38 

W|N 

8 26 

N l E 

98 

26 

E 1 S 

188 26 

S A w 

278 26 

W ! N 

11 15 

N by E 

101 

15 

E by S 

191 15 

S by W 

281 15 

W by N 

14 04 

N by E J E 

104 

04 

ESE f E 

194 04 

S by W J w 

284 04 

WNW f W 

16 53 

N by E | E 

106 

53 

ESE | E 

196 53 

S by W i W 

286 53 

WNW a w 

19 41 

N by E ! E 

109 

41 

ESE a E 

199 41 

S by W f W 

289 41 

WNW 1 W 

22 30 

NNE 

112 

30 

ESE 

202 30 

ssw 

292 30 

WNW 

25 19 

NNE J E 

115 

19 

SE by E | E 

205 19 

SSW 1 w 

295 19 

NW by W f W 

28 08 

NNE i E 

118 

08 

SE by E a E 

208 08 

SSW A w 

298 08 

NW by W a W 

30 56 

NNE |E 

120 

56 

SE by E J E 

210 56 

sswf w 

300 56 

NW by W J W 

33 45 

NE by N 

123 

45 

SE by E 

213 45 

SW by S 

303 45 

NW by W 

36 34 

NE f N 

126 

34 

SE f E 

216 34 

SW! S 

306 34 

NWf W 

39 23 

NE JN 

129 

23 

SE a E 

219 23 

SW A s 

309 23 

NW a w 

42 11 

NE iN 

132 

11 

SE a E 

222 11 

SW A s 

312 11 

NW J W 

45 00 

NE 

135 

00 

SE 

225 00 

SW 

315 00 

NW 

47 49 

NE i E 

137 

49 

SE i S 

227 49 

SW A w 

317 49 

NW J N 

50 38 

NE b S 

140 

38 

SE i S 

320 38 

SW 1 w 

320 38 

NW AN 

53 26 

NE f E 

143 

26 

SE f S 

233 26 

sw f w 

323 26 

NW ! N 

56 15 

NE by E 

146 

15 

SE bv S 

236 15 

SW by W 

326 15 

NW bv N 

59 04 

NEbyEJE 

149 

04 

SSE | E 

239 04 

SW by W A w 

329 04 

NNW ! W 

61 53 

NE by EiE 

151 

53 

SSE § E 

241 53 

SW by W a W 

331 53 

NNW a W 

64 41 

NEbyEf E 

154 

41 

SSE AE 

244 41 

SW by W ! W 

334 41 

NNW a W 

67 30 

ENE 

157 

30 

SSE 

247 30 

WSW 

337 30 

NNW 

70 19 

ENE i E 

160 

19 

S by E f E 

250 19 

WSW a w 

340 19 

N by W ! W 

73 08 

ENE a E 

163 

09 

S by E b E 

253 08 

WSW a w 

343 08 

N by W | W 

75 56 

ENE ! E 

165 

56 

S by E J E 

255 56 

WSW ! W 

345 56 

N by W a W 

78 4 5 

E by N 

168 

45 

S by E 

258 45 

W by S 

348 45 

N by W 

81 34 

EfN 

171 

34 

SfE 

261 34 

Wf S 

351 34 

Nf W 

84 23 

E JN 

174 

23 

S ae 

264 23 

WAS 

354 23 

N|W 

87 11 

E JN 

177 

11 

s A E 

267 11 

WAS 

357 11 

N J W 


Table VII .—Equivalent value in degrees of each fractional division of 
the compass to the nearest minute of arc. 


| point equals 
| point equals 
f point equals 
\ point equals 
f point equals 
f point equals 
l point equals 


1 24 

2 49 

4 13 

5 38 

7 02 

8 26 
9 51 


90245°—19-6 


O 
































—GENERAL ARRANGEMENT PLANS. 






























































































































































































Fig. 9.—GENERAL ARRANGEMENT 
PLANS. 




a '' 5 






<rC : *' 


* 


•4 


.,s 


t* 








FIG. 10.—DIAGRAM OF STRUT NUMBERING. 



















































































Fig. 10.—DIAGRAM OF STRUT 
NUMBERING. 





Terminal 
Pin or Bolt 


^3410 


C otter . 


2629 


Woriher Clin 5pocer s. Nut 


Pm for Shackle or Turnbuckle 22907 

2r»e> 7 

22130 7 

2eso7 

2290-7* 

\ \ 

~*-| \ 

1 v 

1 N 

1 N 

Cotter for ?329 IB 

■10 

iB 

-18 

IB 

1 N 

1 '' 

i > 

1 v 

r - ^ 

Cable No 31-224 

3j-z?S> 

3I2T6 

31*27 


r s 

1 ^ 

1 N 

| N 






\ 


-- 





2390 7 


Pin forTurnbuckk 


Cotter for Turnbuckle Rn 

Terminal __ 

Pin or Bolt 

Cotter __ 

Nut 


2529 


2529 


• ?rs 0-7 

' i v 

-IB 


i ' 
23rze 


3 1687 


31697 

r l 


31692 
1 - 


3)666 
r i 


23-410 



1 

^4C 

y 

1 

7 791 -9 

r ~>— 


-z& 


234/0 

r J— 


23410 

'1 - 



^L3 

, - ^ 

? 70 I 9 

_ _:l& 


2290-7 

7790 7 

2 * 90-7 

2290-7 

r 1 

-ZB 

' 1 

-IP 

' 1 

-IB 

' \ 

IQ 

y 1 

' » 

-IP 

r 7 

1 

'1 

' 1 

r ■ 

'— 1 

nr - 

' 1 

3)221 


3/229 

3/230 


3/231 


3/2 32 

/ ~Z 


' ~ 

< 1 


r / 


' 1 


r-G 




/ 




■J, 






1 

- C* 3 


£5 3 

FRONT 

E -3 

2790-7 

ZZS 7-9 

ggE> 7 < 

* 2237-9 

Z 3439 U 

23 ^ 3^17 

1 ^ 

1 ' 

1 \ 

-2 A 

-IB 

_ -jze 

-Zl 

-28 

-ZC 

•ZC 

1 N 

1 A 

z N 

1 \ 

z N 

1 N 

Z 3 i?e 

1 s 



3 ie> 9 q 



23410 

23410 

23410 

23410 

23410 

234.10 

| \ 

1 \ 

1 \ 

TA 


1 V 

_ 

_ 

- 4 < 

-ha 

- 4 C 

-4 c 

1 ^ 

|A 

1 ^ 

|3 

n 

1 H 


f34344 . 


2 \ 
i 2 c 


2 

31664 


26062’ 


-rc 

1 N 


Z27I II 

fa 


2291-9 

2 s 


-as 
~5 \ 


3)663 

I ' 


227)-II 


23435-1 2 

i \ 

-2C 


I \ 


2271-11 


2291-9 


2 £ 


3290 ) 

2 I 


2406-29 

-SC 

[/ i 

227 III 


2297-)' 


I ^~2 


31666 

' I 


/ r 


2271-1/ 

^ i 






' 1.-4 


25435-12 

2297-3 

2297-9 

/ 5 

r' ' 

' 2 

-2C 

S 2 P 


/ 2 

r 1 

K 2 

31667 

3)695 

3/666 

/ 1 

' 1 

r i 

2606-31 

23410 

23410 

r 1 

✓ | 

^ 1 

- 2 C 

-4C 

-4C 

/ i 

2271-1/ 

u n~ 


2 — 7 — 


REAR 


2291-9 


Ji £5 


3)692 

- 


23410 

- 


-46 


2291-9 
' 2 


r2JB 


3)686 


2291-9 

r—T 






rj 


3)692 




2290-7 


2290-7 

/ i 


j?0 . _UC 


n 

23127 


I 


2jV4IO 234IO 

■) 2 ~ 


ZIO 


23127 

' i 



CMg. 




Washer 

Nut 

Screw 



Incidence Wiring 



249 a-/ 

/ 2 

26040 2560-2 

/ i / 2 — 

2396-10 
/ 2 - 


Sketch 3 howinq Arronqement 
of parts ot f ittinq points 
Scale- Half Size 


Note - 

Number of Ports required shown 

Diaqram is for one hand only- 

Except inq the center (Incidence) Section S' 

which shows Total, and for incidence wirina for Winq Erection See D'We- 6 326 

for section C D sE which shows ^of tota). For EnqmeEquipment see - -6323 

For Streamline Vtirinq see-3121S 


FIG. 11.—WIRING DIAGRAM OF PANELS. 




































































































































































































































































































































































































































































































Pig. 11.—WIRING DIAGRAM OF PANELS 



' 

5 ?" ,v '' tv*3 vo* 

®! - ' r por n r»v -in f :.-nr»0rtC >■ 





























6race .Control 4A&Q 

A 


Front Side- U p per 
Bolf 

NuT 2Z7I-3 

A Cotter 2529-1A 

Gimbal Piece 22-471 
Bolt 256-13 

Nut 2271-3 

(totter 2529-1A 


grace 


ear-Lower 

Boll- 256-17 

Nut 2271-3 

Cotter 23 29 IA 

Gimbal Piece 22471 
BCt 

Nut 2271 3 

Cotter Z529HAI 


Wings 


Brace Control 


Rear U pper 

Bolt-— 

Nut 2271-3 A- 

Cotter 2329-1A 

Gimbal Piece 22471 
Bolt Z56-I3 

Nut 2271-3 

Cotter 25 23-1A 


25C-I 

Z 


front Side - Lower 

Bolt 236-17 

_ Nut 2271-3 

Cotter 25 29HA 

Gimbal Piece 22471 
Bolt 256-13 

I Nut 2271-3 

1 Cotter 2S23 4 A 



Perspective View 


Side Elevation 


Screws 2623-IQL 

TbrK ferwch Streamline 


1 milder must be allaned by eecorud 
hinqe from bottom ono clip on 4: of 


Upper Longeron 


Fitting 31691 I Reed 
Bolt 764-17 2 

Nut 2271- 1 Z 
Cotter-25 29-IA 2 


Z 5 5-21 2 Ree d 

Bolt 25519 2 

Nut 2271-2 4 

C0tfer2529-IA 4- 

Bolt 254-19 

Nut * 22 71-1 4-fte^d 

Cot ter-25 29-IA 


Wi re 32054- 

4 


Wires 32056 


46- 


Wire 32055 


253-21 
255-19 
2271-2 
er-25Z9-IA 


2 Re^'d 


inqePin 2300 
Cotter 2529 IA 7 


Streqm liQB3 ■_ 

Note: Streamlines to be wru 
doped « painted Spec-*SF17 


apped 


Wirsa 


ZMV»(. b 

c>cw3ffoi)5TRLt«ui«\ 2 

4 1 |63 

27\ 2€»Z3 

2491 

WASHER \ | 

° \ 

l 6 ' 


*331 

Z493-12 

SHE.R \ \ 

16 

3271 2> 

*331 

7523U 

COTTE.R 

83 


32t|2; 

5 791 

2Z7I-3 

NUT 

32 

| 6327 Z 

?711 

2771-2 

NUT 

24 

l<E>327 2 

27 11 

2271-1 

NUT 

10 

16327 2 

2711 

Z5e-13| 

BOLT-EVE 

2 

| 

8327 

75S 

250-13 

BOLT. EXE 

2 

I 

fc*5Z7 

238 

756-19 

BOLT 

2 

1 


Z56 

25617 

BOLT 

10 


6327 

256 

29613 

BOLT 

16 


6377 1 

25© 

25534 

BOLT 

16 


6327 

256 

255-15 

bolt 

4 


6327 

25© 

255-21 

bolt 

4 


<8327 

255 

2S4-I9 

bolt 

4 


S327 

254 

294-17 

BOLT 

2 


6327 

254 

2S4-H 

Bolt 

4 


6?27 

254 

32057 

WIRING BRACE 

2 


6327 

32057* 

32056, 

WIRING BRACE 

4 


6327 

320564 

32053 

Wiring brace" 



6327 

32054] 

32054 

WIRING BRACE 

4 


6327 

320541 

32053 

wiring drop 

2 


6327 

32052 

32052 

WIRING DROP 

2 


6327 

3 20521 

32051 

WIRING OfRrFT 

- 2 


6327 

32oSC| 

32050 

wiring drift 

2 


6327 

S205C| 

4671 

3 (Race (Control 

A 


6327 

4671 

4 6 GO 

BRACE (CONTROL 

A 


6327 

46 ed 

4653 

BRACE (CONTROL) 

A 


€>327 

46531 

2296 

PIN (ELEVATOR) 

IO 


©327 

2296* 

2300 

PIN (RUDDER) 

7 


6327 

236C 

22471 

gimbal Piece 

Ife 


6*27 

22471 

32581-9 

STREAMLINE 

4 

TTS- 

fl»t* 

€327 

32381 

J238H7 

.STREAMLINE 

4 

t«« 

63C7 

3238) 

31336 

SRACE(TUSULAR) 

2 


6327 


3*335 

brace (tubular) 

2 


6327 

4297 

31334 

BRACE(TUBULAR) 

2 


C327 

Aar® 7 

31333 

BRACE (TUBULAR) 

2 


6*27 

4 297 

3*891 

FITTING 

1 


6317 

3i&al 

3163! 

fitting 

1 


6327 

31636 

5220 

elevator 

2 


6327 

322o 

5221 

balance: 

1 


*327 

32*1 

522: 

Rudder 

1 


6337 

S 223 

3 5219 
522' 

HOR. STABILIZER 

I 


6327 

3219 

2 VER. STABILIZER 

1 


6327 

52*2 

PART 

* description 

N>Rt 

RNISt 

UStDOl 





-UT-. ^ 



FIG. 12.—TAIL UNIT ASSEMBLY. 
















































































































































































































































































































































































Fig. 12.—TAIL UNIT ASSEMBLY. 

















- 





c s 






























FIG. 13.—LUBRICATION CHART OF MOTOR CONTROL. 
































































































































Fig. 13.—LUBRICATION CHART OF MOTOR 
CONTROL. 







Note 

Appl v drv-yC'l ' - 




t» ves cortnec 


Add I v drop of ^ 


' «n Rudder Mmge s 
Motor Oil 


ppinlS where wre 
nbockles or anochlgA 

■ r oil to ahonk of 


lend* -Qop W.te Grea-y 


I \ i flRirATlQN CHAR T OF SURFACE CONTROL 

riGuwc 


FIG. U.—LUBRICATION CHART OF SURFACE CONTROL. 




















































































Fig. 14.—LUBRICATION CHART OF SURFACE 
CONTROL. 






FIG. 15.—DIAGRAM OF DELCO IGNITION SYSTEM. 


































































































































Fig. 15.—DIAGRAM OF DELCO IGNITION 
SYSTEM. 


MGTOM GjH^Oa. A £ 

























to starboard Motor- 


to <; larbo ard. 

1 Spark Contro l 


Non p/ent>/a cak/v 


o Sfarboart 


3 I 9 S 3 Aesern 

Z SS-lfBott 


Lift Hnrxj Sj*orA Peta rd 2/jTufrybvcMmt 


3707 . 


to bo cross ed a t th/s point S_Q 


fhof spork wi/t be ad*anc.aL 


H-/W fornrord. 


3G.fr of //. Dia tton flexible 


cob/e tor Starboard Throttle control , i 


SlBowdcn So/o Casino* 


Placed t n aiJoSTrooioline 


3/493 


*iQio Assam o,ght Ha nd Thr off It YtlfU ts. 
aoiT-z.-stiff r'rnsso ff nt this point so 

■.<iOi7-S>-at,l/ Ant A throttles // b o. 


32.fi of dzDia Non f/» xi b/e Cable 
[for Port Spark ConTro! 


t 3i 6 garden Solo Casings 


p/actd /noi<dt> Sfream/ine, 


36 ft. of/k Did,Von flexible 


Cab/e for Pori Throtf/t Can-trot, 


''offer 


3/9 S 3 


3136*- '' 

Z 3 S 4 -- 3 C 


Battery Son o faced 


beneath” f> 


jo port throit/e coni rot 


- J- - 

Spark c gnfrol. 


5914 


/Qrurt)?r> Wire 


Condu let 


Turnbuckle 


5+14- 




Cotter 


4402 ,<? 
toot .. ’ A 


S 914 - 


Bolt 


Clip, Tarot Tie 


Ignition 


Wires 


Stock,Guide 


PJ 707 


Guide, Thro tV* 


Guide,Sporh Wire? 


Stiffen er 


Stiffener &ox 


aid a Streamline 


Gutdt, 5pork \Ntre 


of Da/co Ignition System Png 9144 


5414 


Winn# diagram 


+/Q/Q 


Levers > Throt tie. 


Pu I leys , Th rattle 


dip, Throt tie 


ignition Diagram 


dip, kjn. wires 


54 -H 


C/ipjgn Wires 


Rod, CM stribufer, R 


^j \ 3 Turn bu ckle 


For F ngme. Mountirr q s e e 


Switch, 5W off 


Pulley ,5 par k% 


Volt Regulator 


\-GOft d- 


l lQ/0 


Controls.. Motor 


Description 


roriya> 


wtrts can be d/sconf 

e c / ed v/ith the 

L _ diagonal 

rqces. T 


-——r>— ' r 


JJ99.3 


Looking forward 



21674 

La-.-jpi 


o L 


2239-3 

fin 

32 

54 / 4 - 





2 fe /63 

Link 

32 . 

5 -f /-f- 


FIG. 16—WIRING AND MOTOR CONTROLS. 




















































































































































































































































































































































































































































































































































































































































































































































































i 

5 - 

)- 

- 

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Fig. 17—GASOLINE LINES. 
























































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Fig. 57.—ORDNANCE INSTALLATION. 


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